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时间:2011-03-29 09:16来源:蓝天飞行翻译 作者:航空
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 2. Job Set-up Information
______________________
 A. Referenced Information
 -------------------------------------------------------------------------------
REFERENCE DESIGNATION
 -------------------------------------------------------------------------------
AMM 49-00-00-710-004 Operational Test of the APU (4005KM) (GTCP 36-300) AMM 49-51-17-000-001 Removal of the Total Pressure Sensor (8044KM) (GTCP 36-300) AMM 49-51-17-400-001 Installation of the Total Pressure Sensor (8044KM) (GTCP 36-300) AMM 49-51-18-000-001 Removal of the Compressor Inlet-Pressure Sensor (GTCP 36-300) AMM 49-51-18-400-001 Installation of the Compressor Inlet-Pressure Sensor (GTCP 36-300) AMM 49-61-34-000-001 Removal of the Electronic Control Box (ECB) (59KD) (GTCP 36-300) AMM 49-61-34-400-001 Installation of the Electronic Control Box (ECB) (59KD) (GTCP 36-300)
 3. Fault Confirmation
__________________
 A. Do the operational test of the APU (Ref. AMM TASK 49-00-00-710-004).
 4. Fault Isolation
_______________
 A. If the test gives the maintenance message:
 PRESS XDCRS (8044KM) / (8048KM)
 with the LRU TROUBLE SHOOT DATA information:
 TOTAL PRESSURE AND INLET PRESSURE DISAGREE
 Fault Code Number: 027

 - replace the COMPRESSOR INLET PRESSURE TRANSDUCER (8048KM) (Ref. AMM TASK 49-51-18-000-001) and (Ref. AMM TASK 49-51-18-400-001).
 (1) If the fault continues:
 - replace the TOTAL PRESSURE TRANSDUCER (8044KM) (Ref. AMM TASK 49-51-17-000-001) and (Ref. AMM TASK 49-51-17-400-001).
 「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1R EFF : 063-099, 401-499, ∞∞49-00-00∞∞∞∞∞∞∞∞∞∞Page B208
 Config-1 Aug 01/05 CES

 

 (2) If the fault continues:
 - replace the ECB (59KD) (Ref. AMM TASK 49-61-34-000-001) and (Ref. AMM TASK 49-61-34-400-001).
 B. Do the test given in para. 3.

 

R **ON A/C 001-003, 051-099, 401-499,
 TASK 49-00-00-810-863
 Air Intake Actuator Fault (GTCP 36-300)

 1. Possible Causes
_______________
 - AIR INTAKE-FLAP ACTUATOR (4015KM)

 - ECB (59KD)

 - wiring


 2. Job Set-up Information
______________________
 A. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
AMM  49-16-00-710-001 Operational Test of the Air Intake and Diverter (GTCP 36-300) AMM 49-16-51-000-001 Removal of the Air-Intake Flap Actuator (4015KM) (GTCP 36-300) AMM 49-16-51-400-001 Installation of the Air-Intake FLap Actuator (4015KM) (GTCP 36-300) AMM 49-61-34-000-001 Removal of the Electronic Control Box (ECB) (59KD) (GTCP 36-300) AMM 49-61-34-400-001 Installation of the Electronic Control Box (ECB) (59KD) (GTCP 36-300) ASM 49-16/01
 3. Fault Confirmation
__________________
 A. Do the test of the air intake flap-actuator (Ref. AMM TASK 49-16-00-710-001).
 4. Fault Isolation
_______________
 **ON A/C 001-003, 051-062,

 A. If the test gives the maintenance message: AIR INTAKE FLAP ACTR or AIR INTAKE FLAP ACTR OR ECB 59KD: NOTE : The APU SHUTDOWNS report gives the maintenance message:
____

 「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1R EFF : 001-003, 051-099, 401-499, ∞∞49-00-00∞∞∞∞∞∞∞∞∞∞Page B210
 Config-1 Aug 01/05 CES

 

 AIR INTAKE NOT OPEN - AIR INTAKE FLAP ACTR

 - replace the AIR INTAKE-FLAP ACTUATOR (4015KM) (Ref. AMM TASK 49-16-51-000-001) and (Ref. AMM TASK 49-16-51-400-001).
 (1) If the fault continues:

 - replace the ECB (59KD) (Ref. AMM TASK 49-61-34-000-001) and (Ref. AMM TASK 49-61-34-400-001).

 (2) If the fault continues:

 - do a check and repair the wiring from the ECB (59KD) AC/5, 4 to the electrical connector 7527VCA/J, K (Ref. ASM 49-16/01).

 - do a check and repair the wiring from the ECB (59KD) AB/G2, G3, G4, G5 to the electrical connector 7527VCA/D, C, E, B. (Ref. ASM 49-16/01).

 - do a check and repair the wiring from the electrical connector 7527VCA/A, L, F, to the ground (Ref. ASM 49-16/01).

 


R **ON A/C 063-099, 401-499,
 A. If the test gives the maintenance message:
 AIR INTAKE FLAP ACTR (4015KM)
 with the LRU TROUBLE SHOOT DATA menu information:
 INLET FLAP SHOWS FLAP CLOSE CIRCUIT OPEN
 Fault Code Number: 064
 
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